Patents for F01D 11 - Preventing or minimising internal leakage of working fluid, e.g. between stages (10,581) |
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03/05/2015 | WO2015031764A1 Blade outer air seal made of ceramic matrix composite |
03/05/2015 | WO2015031763A1 Seal for gas turbine engine |
03/05/2015 | WO2015031384A1 Bifurcated sliding seal |
03/05/2015 | WO2015030946A1 Gas turbine engine with fan clearance control |
03/05/2015 | WO2015028177A1 Brush seal arrangement |
03/05/2015 | US20150064012 Blade of a rotary flow machine with a radial strip seal |
03/05/2015 | US20150064008 Turbomachine bucket having angel wing for differently sized discouragers and related methods |
03/05/2015 | US20150063990 Turbomachine Axial Compressor Seal with a Brush Seal |
03/05/2015 | US20150063981 Device for sealing between the coaxial shafts of a turbomachine |
03/05/2015 | US20150061228 Sealing arrangement in an axial turbomachine |
03/05/2015 | DE112013002248T5 Aktuatorstangen-Dichtsystem Actuator rods sealing system |
03/05/2015 | DE102013217581A1 Dichtungsanordnung in einer axialen Strömungsmaschine Seal assembly in an axial flow machine |
03/04/2015 | EP2843198A1 Method and control system for active rotor tip control clearance |
03/04/2015 | EP2843197A2 Blade of a rotary flow machine with a radial strip seal |
03/04/2015 | EP2843196A1 Compressor of an axial turbomachine with brush seal and corresponding turbomachine |
03/03/2015 | US8970228 Rotational clearance measurement system and method of operation |
03/03/2015 | US8967974 Composite airfoil assembly |
03/03/2015 | US8967973 Turbine bucket platform shaping for gas temperature control and related method |
03/03/2015 | US8967957 Rotating airfoil component of a turbomachine |
03/03/2015 | US8967955 Turbocharger with variable nozzle having labyrinth seal for vanes |
03/03/2015 | US8967627 Intershaft seal |
02/26/2015 | WO2015026534A1 Belly band seal with circumferential spacer |
02/26/2015 | US20150056068 Belly band seal with circumferential spacer |
02/26/2015 | US20150054362 Method and Device for Sensorless Control of a Separately Excited Synchronous Machine |
02/26/2015 | DE112013001882T5 Axialturbine mit Sicherheitsummantelung Axial turbine with protective enclosure |
02/26/2015 | DE102013210876B4 Verbundbauteil zur thermischen Spaltsteuerung in einer Strömungsmaschine sowie dieses enthaltende Strömungsmaschine Composite component for thermal gap control in a turbomachine, and this flow containing machine |
02/25/2015 | EP2840229A1 Flow guide within a steam turbine seal |
02/25/2015 | EP2839117A1 Turbine stage for a turbomachine |
02/24/2015 | US8961151 Turbocharger |
02/24/2015 | US8961137 Turbine wheel for a turbine engine |
02/24/2015 | US8961135 Mateface gap configuration for gas turbine engine |
02/24/2015 | US8961132 Secondary flow arrangement for slotted rotor |
02/24/2015 | US8961117 Insulating a circumferential rim of an outer casing of a turbine engine from a corresponding ring sector |
02/24/2015 | US8961115 Clearance control for gas turbine engine seal |
02/24/2015 | CA2598259C Simple axial retention feature for abradable members |
02/19/2015 | WO2015023471A1 Flow vortex spoiler |
02/19/2015 | WO2015023321A2 Radial position control of case supported structure with axial reaction member |
02/19/2015 | US20150050151 Annulus filler |
02/19/2015 | US20150050150 Annulus filler |
02/19/2015 | US20150050138 Fixation device for turbine and method for applying fixation |
02/19/2015 | US20150050130 Sealing device between two axisymmetric coaxial parts |
02/19/2015 | US20150050127 Air with integral spring for a gas turbine engine exhaust drive |
02/19/2015 | US20150050125 Fluid seal arrangement and method for constricting a leakage flow through a leakage gap |
02/19/2015 | US20150048618 Turbine generator |
02/19/2015 | US20150047356 Turbine engine, such as a turbojet or a turboprop engine |
02/19/2015 | DE102013216400A1 Leitschaufel mit einer Borsten umfassenden Dichteinrichtung Vane with a comprehensive bristles sealing device |
02/18/2015 | EP2837860A1 Brush seal |
02/18/2015 | EP2837858A1 Brush seal |
02/18/2015 | EP2837774A1 Annulus filler and corresponding stage and gas turbine engine |
02/18/2015 | EP2837773A1 Annulus filler and corresponding stage and gas turbine engine |
02/18/2015 | EP2837772A1 Annulus filler and corresponding stage and gas turbine engine |
02/18/2015 | EP2836684A1 Turbine engine, such as a turbojet or a turboprop engine |
02/17/2015 | US8956120 Non-continuous ring seal |
02/17/2015 | US8956106 Adaptive eductor system |
02/17/2015 | US8956104 Bucket assembly for turbine system |
02/12/2015 | WO2015021247A1 High porosity abradable coating |
02/12/2015 | WO2015021222A1 Clearance control assembly |
02/12/2015 | WO2015021029A1 Boas with radial load feature |
02/12/2015 | WO2015020775A1 Gas turbine engine aft seal plate geometry |
02/12/2015 | WO2015020708A2 Gas turbine rapid response clearance control system with annular piston |
02/12/2015 | WO2015018841A1 Insert element, ring segment, gas turbine, mounting method |
02/12/2015 | WO2015018839A1 Insert element, ring segment, gas turbine, and assembly method |
02/12/2015 | US20150044035 High porosity abradable coating |
02/12/2015 | US20150044018 Active seal system |
02/12/2015 | US20150040567 Systems and Methods for Reducing or Limiting One or More Flows Between a Hot Gas Path and a Wheel Space of a Turbine |
02/12/2015 | US20150040566 Helical seal system for a turbomachine |
02/12/2015 | DE102014111201A1 Systeme und Verfahren zur Reduktion oder Beschränkung einer oder mehrerer Strömungen zwischen einem Heißgaspfad und dem Rotorinnenraum einer Turbine Systems and methods for the reduction or limitation of one or more flows between a hot gas path and the rotor interior of a turbine |
02/12/2015 | DE10140742B4 Vorrichtung zur Dichtspaltreduzierung zwischen einer rotierenden und einer stationären Komponente innerhalb einer axial durchströmten Strömungsmaschine A device for sealing gap reduction between a rotating and a stationary component in an axial-flow turbomachine |
02/11/2015 | EP2835504A1 Insert element and gas turbine |
02/11/2015 | EP2835502A2 Blade of a turbine |
02/11/2015 | EP2835500A1 Insert element and gas turbine |
02/11/2015 | EP2834502A1 Axial non-contact seal |
02/11/2015 | CN104350238A 覆盖有耐磨涂层的涡轮机定子壁 Covered with a wear-resistant coating of turbine stator wall |
02/11/2015 | CN104343473A 一种用于有机工质向心透平的轴端密封装置 A shaft sealing device to the heart of the organic working fluids for turbine |
02/11/2015 | CN104343472A 具有改进的密封的涡轮叶片和涡轮 Having improved sealing of the turbine blades and turbine |
02/10/2015 | US8951014 Turbine blade with mate face cooling air flow |
02/10/2015 | US8951008 Compressor blade and production and use of a compressor blade |
02/10/2015 | US8950751 Compliant element |
02/05/2015 | WO2015017040A2 Gas turbine engine vane ring arrangement |
02/05/2015 | US20150037145 Systems relating to axial positioning turbine casings and blade tip clearance in gas turbine engines |
02/05/2015 | US20150037142 Casing for turbomachine blish and turbomachine equipped with said casing |
02/05/2015 | US20150037133 System and method relating to axial positioning turbine casings and blade tip clearance in gas turbine engines |
02/05/2015 | DE102014110749A1 Systeme und Verfahren betreffend die axiale Positionierung von Turbinengehäusen und den Schaufelspitzenspalt in Gasturbinen Systems and procedures concerning the axial positioning of turbine housings and the blade tip clearance in gas turbines |
02/04/2015 | EP2832975A1 Seal member, turbine, and gas turbine |
02/04/2015 | EP2832952A1 Turbine blade and turbine with improved sealing |
02/04/2015 | EP2831380A1 Knife edge seal for gas turbine engine |
02/04/2015 | EP2831376A1 Turbine blade |
02/04/2015 | CN204140141U 主动控制叶尖间隙的执行机构和系统 Active tip clearance control actuators and systems |
02/04/2015 | CN204140140U 一种用于燃气轮机封严的止扣环结构 Only grommet seal structure for a gas turbine of |
02/04/2015 | CN104329125A 燃气轮机 Gas turbine |
02/03/2015 | US8944762 Spoked spacer for a gas turbine engine |
02/03/2015 | US8944756 Blade outer air seal assembly |
02/03/2015 | US8944751 Turbine nozzle cooling assembly |
01/29/2015 | WO2015013503A1 Trough seal for gas turbine engine |
01/29/2015 | WO2015013114A1 Turbocharger purge seal including axisymmetric supply cavity |
01/29/2015 | WO2015010740A1 Sealing arrangement for a turbomachine |
01/29/2015 | US20150030826 Method for creating a textured bond coat surface |
01/29/2015 | US20150030442 Seal member, turbine, and gas turbine |
01/29/2015 | US20150030433 Method and apparatus for measuring turbine shell clearance |
01/28/2015 | EP2829689A1 Insulating structure for a thermal gas turbine, coresponding thermal gas turbine and method of manufacturing |